nach oben

Experiments in Fluids

Erschienen in:

01.01.2014 | Research Article

On the laminar-turbulent transition in injection-driven porous chambers

verfasst von: B. Gazanion, F. Chedevergne, G. Casalis

Erschienen in: Experiments in Fluids | Ausgabe 1/2014

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config

KI-gestützte Suche

Aus

Abstract

This paper presents a characterization of the laminar-turbulent transition in a cold flow setup, representative of the flow in a solid rocket motor. Recent developments based on a linear stability analysis of this particular flow have highlighted the existence of intrinsic instabilities, generating the so-called parietal vortex shedding, responsible for thrust oscillations. From this essential ingredient, an original interpretation of the laminar-turbulent transition is proposed using three approaches. Eventually, a description of the laminar and turbulent areas is obtained for the entire flow, from which a transition line is defined.

Vorheriger Artikel Laser diagnostics of an evaporating electrospray

Nächster Artikel Tomographic PIV measurements of flow patterns in a nasal cavity with geometry acquisition

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

über 102.000 Bücher
über 537 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Finance + Banking
Management + Führung
Marketing + Vertrieb
Maschinenbau + Werkstoffe
Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

über 67.000 Bücher
über 390 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Maschinenbau + Werkstoffe

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Poral bronze, made of sintered small bronze spheres.

Up to four packets of harmonics are visible on Fig. 8b.

Instead of 40 samples of duration equals to 2.475 × 10⁻² s.

By definition \(\hat{u}=\frac{U-\mu}{\sigma}\); here \(\mu=\overline{U}\) is the mean, so U − μ = u, and σ = u _rms is the standard deviation of U.

Apte S, Yang V (2003) A large-eddy simulation study of transition and flow instability in a porous-walled chamber with mass injection. J Fluid Mech 477:215–225CrossRefMATH

Arnal D, Juillen JC (1977) Étude de l’intermittence dans une région de transition de la couche limite. La Recherche Aérospatiale 3:147–166

Avalon G, Josset T (2006) Cold gas experiments applied to the understanding of aeroacoustic phenomena inside solid propellant boosters. AIAA

Avalon G, Ugurtas B, Grisch F, Bresson A (2000) Numerical computations and visualization tests of the flow inside a cold gas simulation with characterization of a parietal vortex shedding. AIAA, Huntsville

Ballereau S, Godfroy F, Gallier S, Orlandi O, Thepenier J, Robert E, Cesco N (2011) Evaluation method of thrust oscillations in large SRM—application to segmented SRM’s. In: AIAA Paper 2011-6054

Berman A (1953) Laminar flow in channel with porous walls. J Appl Phys 24(9):1232–1235

Boyer G, Casalis G, Estivalezes JL (2012) Theoretical investigation of the parietal vortex shedding in solid rocket motors. AIAA, Atlanta

Brown RS, Dunlap R, Young SW, Waugh RC (1981) Vortex shedding as a source of acoustic energy in segmented solid rockets. J Spacecr Rockets 18: 312–319. doi:10.2514/3.57822 CrossRef

Casalis G, Avalon G, Pineau JP (1998) Spatial instability of planar channel flow with fluid injection through porous walls. Phys Fluid 10:2558. doi:10.1063/1.869770 CrossRefMATHMathSciNet

Chedevergne F, Casalis G (2005) Thrust oscillations in reduced scale solid rocket motors, part II : a theoretical approach. In: AIAA Paper 2005-4000

Chedevergne F, Casalis G (2006) Detailed analysis of the thrust oscillations in reduced scale solid rocket motors. AIAA, Sacramento

Chedevergne F, Casalis G (2006) Front wall boundary layer influence on the stability of the flow induced by wall injection. In: ONERA-DLR aerospace symposium

Chedevergne F, Casalis G, Féraille T (2006) Biglobal linear stability analysis of the flow induced by wall injection. Phys Fluid 18(1):014,103–14

Chedevergne F, Casalis G, Majadalani J (2012) Direct numerical simulation and biglobal stability investigations of the gaseous motion in solid rocket motors. J Spacecr Rockets 706:190–218CrossRefMATHMathSciNet

Culick FEC (1966) Rotational axisymmetric mean flow and damping of acoustic waves in a solid propellant rocket. AIAA J 4(8):1462–1464CrossRefMATH

Dunlap R, Blackner AM, Waugh RC, Brown RS, Willoughby PG (1990) Internal flow field studies in a simulated cylindrical port rocket chamber. J Propuls Power 6:690–704CrossRef

Flandro GA, Majdalani J (2003) Aeroacoustic instability in rockets. AIAA J 41(3):485–497. doi:10.2514/2.1971 CrossRef

Griffond J, Casalis G, Pineau J (2000) Spatial instability of flow in a semiinfinite cylinder with fluid injection through its porous walls. Eur J Mech B Fluids 19(1):69–88CrossRefMATH

Prévost M, Godon JC (2005) Thrust oscillations in reduced scale solid rocket motors, part I : experimental investigations. In: AIAA Paper 2005-4003

Taylor GI (1956) Fluid flow in regions bounded by porous surfaces. Proc R Soc Lond Ser A Math Phys Sci 234(1199):456–475. doi:10.1098/rspa.1956.0050 CrossRefMATH

Traineau JC, Hervat P, Kuentzmann P (1986) Cold-flow simulation of a two-dimensional nozzleless solid rocket motors. In: AIAA Paper 86-1447

Vuillot F (1995) Vortex shedding phenomena in solid propellant motors. J Propuls Power 11(4):626–639CrossRef

Yagodkin VI (1967) Use of channels with porous walls for studying flows which occur during combustion of solid propellants. In: Proceedings of the 18th international astronautical congress, vol 3, pp 67–79

Yildiz D, Anthoine J, Buchlin JM (2001) Influence of radial injected flow on the aeroacoustic coupling in solid propellant boosters. Am Inst Aeronaut Astronaut. doi:10.2514/6.2001-2101

Titel: On the laminar-turbulent transition in injection-driven porous chambers
verfasst von: B. Gazanion
F. Chedevergne
G. Casalis
Publikationsdatum: 01.01.2014
Verlag: Springer Berlin Heidelberg
Erschienen in: Experiments in Fluids / Ausgabe 1/2014
Print ISSN: 0723-4864
Elektronische ISSN: 1432-1114
DOI: https://doi.org/10.1007/s00348-013-1643-y

Premium Partner

Marktübersichten

Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.

Zur Marktübersicht

Springer Professional

Abstract

Bitte loggen Sie sich ein, um Zugang zu Ihrer Lizenz zu erhalten.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Springer Professional "Technik"

Weitere Artikel der Ausgabe 1/2014

On the appropriate filtering of PIV measurements of turbulent shear flows

Analysis of three-dimensional attributes and flow intake for an oscillating cantilever

The onset of cavitation during the collision of a sphere with a wetted surface

Experimental investigation of the inclined interface Richtmyer–Meshkov instability before and after reshock

PIV experiments in rough-wall, laminar-to-turbulent, oscillatory boundary-layer flows

Measurements about the air motion in an acoustically forced jet: effects of the dispersed phase on the coherent flow structure

Premium Partner

Marktübersichten